Invention Grant
- Patent Title: Method for manufacturing a stiffened panel made from composite material
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Application No.: US15427194Application Date: 2017-02-08
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Publication No.: US10549490B2Publication Date: 2020-02-04
- Inventor: Pedro Nogueroles Viñes , Jose Cuenca Rincón , Aquilino Garcia Garcia , Bernardo Lopez Romano , Maria Mora Mendias
- Applicant: Airbus Defence and Space S.A.
- Applicant Address: ES Getafe
- Assignee: AIRBUS DEFENCE AND SPACE S.A.
- Current Assignee: AIRBUS DEFENCE AND SPACE S.A.
- Current Assignee Address: ES Getafe
- Agency: Greer, Burns & Crain, Ltd.
- Priority: EP16382052 20160209
- Main IPC: B29C70/34
- IPC: B29C70/34 ; B29C70/38 ; B29C70/54 ; B29K105/06 ; B29K307/04 ; B29L9/00 ; B29L31/30

Abstract:
A method for manufacturing a stiffened panel made from composite material comprising a skin and elongated reinforcing elements wherein some of the elongated reinforcing elements cross each other. The method comprises the steps of (a) laying up a flat laminate comprising stacked plies of composite layers for forming a structure comprising the elongated reinforcing elements of the panel, (b) cutting the flat laminate along intersection lines of planes defining the webs of two crossing reinforcing elements, (c) cutting in the flat laminate the outline of the elongated reinforcing elements, (d) forming the structure comprising the elongated reinforcing elements of the panel, (e) laying up plies of composite layers for forming the skin, and (f) curing the laid-up plies of the skin and the formed structure comprising the elongated reinforcing elements.
Public/Granted literature
- US20170225406A1 METHOD FOR MANUFACTURING A STIFFENED PANEL MADE FROM COMPOSITE MATERIAL Public/Granted day:2017-08-10
Information query
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